The testing of a titanium matrix composite (TMC) F-15 nose gear outer cylinder is discussed. Two cylinders were fabricated. An entire F-15 nose gear was assembled using the first cylinder. This test gear underwent static structural tests to three critical loading conditions and functional evaluations including load-stroke, rebound snubbing, jig drops and strut stroke cycling. The TMC cylinder successfully completed both groups of testing with no signs of structural or functional degradation.


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    Titel :

    Testing of a Titanium Matrix Composite Landing Gear


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Morris, David L. (Autor:in) / Shea, Mark A. (Autor:in) / Macy, William W. (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 1991



    Erscheinungsdatum :

    1991-09-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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